| Number |
2011-0205R1 |
| Issued by |
 Europe |
| Issue date |
2017-02-07 |
| Effective date |
2017-01-30 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
|
| Revision |
This AD revises EASA AD 2011-0205 dated 13 October 2011.
|
| Correction |
This AD is republished to correct the affected Tail Fin Assembly P/N.
|
| Supersedure |
The original issue of this AD superseded EASA AD 2006-0358R1 dated 28 September 2011.
|
| Publication(s) and related information |
Agusta MM 39-A-AMPI-00-P Chapter IV Issue 2 Change 12, or Leonardo S.p.A Helicopters 39-A-AMPI-00-P Chapter IV Issue 7.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
